For the selected UT time-interval the co-ordinates of spacecraft are shown with 10-min step. For each moment the date and time are shown in format as follows:
UTYYMMDD HHMNSS - Date (YYYYMMDD) and UT (hhmmss)
for each moment in the columns the following information is shown:
REG - the geomagnetic region in the spacecraft position, R (Earth's radii) - the spacecraft geocentric distance, Rx = sqrt(Ygse X Ygse + Zgse X Zgse) - the spacecraft distance from Xgse axis, Xgse (Earth's radii) - SC position Ygse (Earth's radii) - in the Zgse (Earth's radii) - SE C/S, Ygsm (Earth's radii) - (Xgsm = Xgse) SC position in the Zgsm (Earth's radii) - GSM C/S GMLAT (deg) - the spacecraft geomagnetic latitude, GMLT (h) - the spacecraft geomagnetic local time, CORLAT (deg) - the corrected geomagnetic latitude, CORMLT (h) - the corrected geomagnetic local time
In case any of the mentioned parameters is not determined, 99.99 replace its value.
The region designations used in the numerical files.
The simulative geophysical region models.